# STC SA00483SE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Arrow Falcon by Edgefield Manufacturing, United States
- Description: Replacement of the original windshields, chin bubbles, skylights, and door windows
- Applied: October 29, 1997
- Status date: May 14, 2024
- Product: Aircraft, Rotorcraft
- Certification basis: Part 21
- Data sheets: [TCDS H22NM](https://openairdocs.org/tcds/H22NM)
- Certificate PDF: https://openairdocs.org/files/sha256/74/96/74968780b02970f7f1c686e984fdacbe9e176b4407de324b5a10d575c9ded4ba
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130775844520240516151633.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00483SE

## ADs that name it (0)

None.

## Approved models (3)

- Arrow Falcon by Edgefield Manufacturing OH-58A ([TCDS H22NM](https://openairdocs.org/tcds/H22NM))
- Arrow Falcon by Edgefield Manufacturing OH-58A+ ([TCDS H22NM](https://openairdocs.org/tcds/H22NM))
- Arrow Falcon by Edgefield Manufacturing OH-58C ([TCDS H22NM](https://openairdocs.org/tcds/H22NM))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

FAA Form 8110-2 (03/21) FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION FAA Form 8110-2 (4/20) SUPERSEDES PREVIOUS EDITION Page 1 of 2

Number: SA00483SE Arrow Falcon by Edgefield Manufacturing 27400 Southeast Nelson Road PO Box 429 Sandy, Oregon 97055 Sandy Oregon 97055

Part 21.25 (a)(2) of the Federal Aviation Regulations.

Original Product Make: Arrow Falcon by Edgefield Manufacturing Type Certificate Number: H22NM Model: OH-58A, OH-58A+, and OH-58C (Restricted Category Only)

Description of Type Design Change: Replacement of the original windshields, chin bubbles, skylights, and door windows with Arrow Falcon Exporters, Inc. parts fabricated and installed in accordance with Arrow Falcon Exporters, Inc. Master Drawing List (MDL) No. 971703, Revision “C”, dated November 17, 1997, or later Federal Aviation Administration (FAA) approved revision. These replacement parts must be maintained in accordance with U.S. Army Aviation Unit and Intermediate Maintenance Manual, OH-58A and OH-58C Helicopters, Paragraphs 2-123 through 2- 128, dated May 25, 1984, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to the above noted model rotorcraft only.

This approval should not be extended to other rotorcraft of these models on which other previously approved modifications are incorporated, unless it is determined by the installer that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that rotorcraft. A copy of this certificate must be maintained as part of the permanent records for the modified aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of Application: October 29, 1997 Date Reissued: April 11, 2024; May 14, 2024

Date of Issuance: November 21, 1997 Date Amended:

Title: For Gregory S. DiLibero Branch Manager, West Certification Branch Compliance and Airworthiness Division Aviation Safety

The STC’s supporting documentation (drawings, instructions,

FAA Form 8110-2 (03/21) specifications, flight manual supplements, etc.) is the property of the STC holder.

Number: SA00483SE

## Every issue (2)

- May 14, 2024: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/74/96/74968780b02970f7f1c686e984fdacbe9e176b4407de324b5a10d575c9ded4ba)
- November 21, 1997: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/98/f1/98f1a655b0d34b6bf087ca63222d31dbe79e6ff20361638318df45c15bf9b6ed)

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